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Design of Entry Trajectory Tracking Law for a Hypersonic Vehicle via Inversion Control
Zhiqiang Pu; Xiangmin Tan; Guoliang Fan; Jianqiang Yi
2012
会议名称The 10th World Congress On Intelligent Control and Automation
会议录名称Proceedings of the 10th World Congress On Intelligent Control and Automation
会议日期July 6-8, 2012
会议地点Beijing China
摘要A nominal altitude-velocity longitudinal entry trajectory is planned and tracked for a Generic Hypersonic Vehicle (GHV) in this paper. The entry corridor is presented which is defined by the dynamic pressure, normal acceleration, heating constraints, and the so-called Quasi-Equilibrium Glide Condition (QEGC). The flyability of the vehicle along the nominal trajectory is carefully analyzed for further validation of the selected nominal trajectory. The control scheme mainly consists of two loops: a guidance loop and an attitude loop, of which the latter is separated into the slow and fast loops with the time-scale separation theory. Inversion control is employed in these three loops, and an integration feedback approach is especially added into the inversion controller to eliminate the tracking error. Simulations demonstrate that the nominal trajectory is designed appropriately and tracked well.
关键词Hypersonic Vehicle Entry Trajectory Tracking Inversion Control Integration Feedback
收录类别EI
文献类型会议论文
条目标识符http://ir.ia.ac.cn/handle/173211/12359
专题综合信息系统研究中心
通讯作者Zhiqiang Pu
作者单位Institute of Automation, Chinese Academy of Sciences
推荐引用方式
GB/T 7714
Zhiqiang Pu,Xiangmin Tan,Guoliang Fan,et al. Design of Entry Trajectory Tracking Law for a Hypersonic Vehicle via Inversion Control[C],2012.
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